Flight Reconstruction of Plume-Induced Site Alteration from InSight
The understanding of rocket plume–surface interaction on planetary bodies will drive safer and more sustainable exploration missions. To that end, the average plume-induced erosion rate of the Mars InSight lander during its powered descent was estimated at 60.4 kg/s. The volume of material displace...
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Veröffentlicht in: | Journal of spacecraft and rockets 2021-05, Vol.58 (3), p.879-893 |
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description | The understanding of rocket plume–surface interaction on planetary bodies will drive safer and more sustainable exploration missions. To that end, the average plume-induced erosion rate of the Mars InSight lander during its powered descent was estimated at 60.4 kg/s. The volume of material displaced and final form of the site were reconstructed photogrammetrically using postlanding images captured by the Instrument Deployment Camera. The resulting elevation model shows six craters of ranging sizes, with an average maximum depth of 15 cm. Other inputs to the erosion computation included estimates of plume impingement time and the bulk density of the regolith at the landing site, Elysium Planitia. An analysis characterizing the erosion physics and uncertainty propagation are noted within this paper, along with other related observations. To better estimate erosion rate, future missions should include a descent imager whose time series of images would simultaneously provide transient elevation models and improved estimates of the impingement time. |
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To that end, the average plume-induced erosion rate of the Mars InSight lander during its powered descent was estimated at 60.4 kg/s. The volume of material displaced and final form of the site were reconstructed photogrammetrically using postlanding images captured by the Instrument Deployment Camera. The resulting elevation model shows six craters of ranging sizes, with an average maximum depth of 15 cm. Other inputs to the erosion computation included estimates of plume impingement time and the bulk density of the regolith at the landing site, Elysium Planitia. An analysis characterizing the erosion physics and uncertainty propagation are noted within this paper, along with other related observations. To better estimate erosion rate, future missions should include a descent imager whose time series of images would simultaneously provide transient elevation models and improved estimates of the impingement time.</description><identifier>ISSN: 0022-4650</identifier><identifier>EISSN: 1533-6794</identifier><identifier>DOI: 10.2514/1.A34935</identifier><language>eng</language><publisher>Reston: American Institute of Aeronautics and Astronautics</publisher><subject>Bulk density ; Descent ; Elevation ; Erosion rates ; Image reconstruction ; Impingement ; Mars missions ; Plains ; Regolith</subject><ispartof>Journal of spacecraft and rockets, 2021-05, Vol.58 (3), p.879-893</ispartof><rights>This material is declared a work of the U.S. Government and is not subject to copyright protection in the United States. All requests for copying and permission to reprint should be submitted to CCC at ; employ the eISSN to initiate your request. 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To that end, the average plume-induced erosion rate of the Mars InSight lander during its powered descent was estimated at 60.4 kg/s. The volume of material displaced and final form of the site were reconstructed photogrammetrically using postlanding images captured by the Instrument Deployment Camera. The resulting elevation model shows six craters of ranging sizes, with an average maximum depth of 15 cm. Other inputs to the erosion computation included estimates of plume impingement time and the bulk density of the regolith at the landing site, Elysium Planitia. An analysis characterizing the erosion physics and uncertainty propagation are noted within this paper, along with other related observations. To better estimate erosion rate, future missions should include a descent imager whose time series of images would simultaneously provide transient elevation models and improved estimates of the impingement time.</description><subject>Bulk density</subject><subject>Descent</subject><subject>Elevation</subject><subject>Erosion rates</subject><subject>Image reconstruction</subject><subject>Impingement</subject><subject>Mars missions</subject><subject>Plains</subject><subject>Regolith</subject><issn>0022-4650</issn><issn>1533-6794</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>2021</creationdate><recordtype>article</recordtype><recordid>eNpl0MFLwzAUBvAgCs4p-CcURPDSmZeXtM1xDKeDgeL0HNIs0Y6umUl68L_fZgUPnt7l974PPkKugU6YAH4PkylyieKEjEAg5kUp-SkZUcpYzgtBz8lFjBtKoagKOSKzedt8fKbs1RrfxRR6kxrfZd5lL22_tfmiW_fGrrNVk2w2bZMN-ge44LfZolsdny_JmdNttFe_d0ze5w9vs6d8-fy4mE2XuWZAU86hlpW2EnVpDMOKM-FKDtLIWiKvXA0owGElAanlpgJJOVrHa6ipkxpwTG6G3F3wX72NSW18H7pDpWICKeUlK9lB3Q3KBB9jsE7tQrPV4VsBVceJFKhhogO9HahutP4L--f2yEph7w</recordid><startdate>202105</startdate><enddate>202105</enddate><creator>Manginelli, Michael S</creator><creator>Mehta, Manish</creator><creator>Thomas, Orrin H</creator><general>American Institute of Aeronautics and Astronautics</general><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>L7M</scope></search><sort><creationdate>202105</creationdate><title>Flight Reconstruction of Plume-Induced Site Alteration from InSight</title><author>Manginelli, Michael S ; Mehta, Manish ; Thomas, Orrin H</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-a210t-41b98ae93a7cc238425f7419c9b9348fb1351f389130e4c819043ef4b1b0f9a13</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>2021</creationdate><topic>Bulk density</topic><topic>Descent</topic><topic>Elevation</topic><topic>Erosion rates</topic><topic>Image reconstruction</topic><topic>Impingement</topic><topic>Mars missions</topic><topic>Plains</topic><topic>Regolith</topic><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Manginelli, Michael S</creatorcontrib><creatorcontrib>Mehta, Manish</creatorcontrib><creatorcontrib>Thomas, Orrin H</creatorcontrib><collection>CrossRef</collection><collection>Mechanical & Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Journal of spacecraft and rockets</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Manginelli, Michael S</au><au>Mehta, Manish</au><au>Thomas, Orrin H</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Flight Reconstruction of Plume-Induced Site Alteration from InSight</atitle><jtitle>Journal of spacecraft and rockets</jtitle><date>2021-05</date><risdate>2021</risdate><volume>58</volume><issue>3</issue><spage>879</spage><epage>893</epage><pages>879-893</pages><issn>0022-4650</issn><eissn>1533-6794</eissn><abstract>The understanding of rocket plume–surface interaction on planetary bodies will drive safer and more sustainable exploration missions. 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subjects | Bulk density Descent Elevation Erosion rates Image reconstruction Impingement Mars missions Plains Regolith |
title | Flight Reconstruction of Plume-Induced Site Alteration from InSight |
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